AH-7-47-6 AIRFOIL

Thickness: 5.9%
Camber: 6.2%
Trailing edge angle: 21.8o
Lower flatness: 7.0%
Leading edge radius: 2.0%
Efficiency: 42.2
Max CL: 1.783
Max CL angle: 7.5
Max L/D: 60.586
Max L/D angle: 0.5
Max L/D CL: 0.992
Stall angle: 7.5
Zero-lift angle: -8.0